An applicable testability framework for small satellite under the operational response space

Peng Lin, Xuetao Tian, Xiaojuan Wang, Jingmin Liu, Jianli Li, J. Le
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Abstract

Focused on the significant features such as highly integration, flexible assembly and rapid testability of small satellite under the operational response space (SSUORS), an applicable framework of design for testability (DFT) is proposed to assure the testability of the SSUORS system. A combined structure of the DFT framework is presented to assure the system-level testability. Further, three patterns of extended build-in test are proposed to enhance the function-level testability, which are specified as additional testability requirements. In addition, both simple and complex scenario-based assignment test models are established based on the proposed DFT framework respectively. Compared with the traditional DFT, more complicated test requirements can be realized sufficiently, and more flexible test strategies can be implemented conveniently by the proposed DFT framework.
一种适用于运行响应空间下的小卫星可测试性框架
针对小卫星在作战响应空间(SSUORS)下高度集成、装配灵活、快速可测试性等显著特点,提出了一种适用的可测试性设计框架(DFT),以保证SSUORS系统的可测试性。为了保证系统级的可测试性,提出了DFT框架的组合结构。在此基础上,提出了三种扩展内嵌测试模式以提高功能级的可测试性,并将其作为附加的可测试性要求加以说明。此外,基于所提出的DFT框架分别建立了简单和复杂的基于场景的分配测试模型。与传统的DFT相比,该DFT框架可以充分实现更复杂的测试需求,并方便地实现更灵活的测试策略。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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